An exemplary boundary layer ingestion engine (300) includes a gas generator (310), a turbine (320) fluidly connected to the gas generator (310), and a fan (330) mechanically linked to the turbine (320) via at least one shaft (340). The linkage is configured such that rotation of the turbine (320) is translated to the fan (330). The boundary layer ingestion engine (300) further includes an exhaust duct fluidly connected to an outlet of the turbine (320). The exhaust duct is positioned radially inward of the fan (330).


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    Title :

    AFT FAN COUNTER-ROTATING TURBINE ENGINE


    Additional title:

    GEGENLÄUFIGES HECKLÜFTERTURBINENTRIEBWERK
    MOTEUR À TURBINE CONTRAROTATIF DE SOUFFLANTE ARRIÈRE


    Contributors:

    Publication date :

    2020-08-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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